Grid Generation -- Hybrid unstructured Grid Generation in MEGAFLOW -- Structured Solver FLOWer -- Block Structured Navier-Stokes Solver FLOWer -- Transition Modeling in FLOWer - Transition Prescription and Prediction -- Turbulence Models in FLOWer -- Hybrid Solver TAU -- Overview of the Hybrid RANS Code TAU -- Algorithmic Developments in TAU -- Hybrid Grid Adaptation in TAU -- Turbulence Model Implementation in TAU -- G.I.G. - A Flexible User-Interface for CFD-Code Configuration Data -- Validation -- Computation of Aerodynamic Coefficients for Transport Aircraft with MEGAFLOW -- Computation of Engine-Airframe Installation Drag -- Verification of MEGAFLOW-Software for High Lift Applications -- Shape Optimization -- The Continuous Adjoint Approach in Aerodynamic Shape Optimization -- Application of the Adjoint Technique with the Optimization Framework Synaps Pointer Pro -- Shape Parametrization Using Freeform Deformation -- Contributions of Universities -- Advanced Turbulence Modelling in Aerodynamic Flow Solvers -- Large-Eddy Simulation of Attached Airfoil Flow -- Transition Prediction for 2D and 3D Flows using the TAU-Code and N-Factor Methods -- Exploitation of MEGAFLOW Software -- Application of the MEGAFLOW Software at DLR -- MEGAFLOW for AIRBUS-D - Applications and Requirements -- Aerodynamic Analysis of Flapping Airfoil Propulsion at Low Reynolds Numbers.